Airworthiness Directive

AD 98-21-05 Amendment 39-10813

Federal Aviation Administration · 14 CFR part 39

FR document
98-26392
Amendment
39-10813
Published
1998-10-06
Models covered
1
Last live check
Not yet re-verified
AD

98-21-05

FR doc 98-26392

AD 98-21-05Published 1998-10-06Effective 1998-11-10

Requires repetitive visual inspections of the flap levers and bracket assembly of the inner flap sub-assembly of the left and right wings to detect certain discrepancies; and corrective actions, if necessary.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to all SD3-30, SD3-60, SD3-60 SHERPA, and SD3 SHERPA series airplanes, that requires repetitive visual inspections of the flap levers and bracket assembly of the inner flap sub-assembly of the left and right wings to detect certain discrepancies; and corrective actions, if necessary. This amendment is prompted by mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to detect and correct failure of the levers and bracket assembly, which could result in uncommanded retraction of the inner flap assembly and consequent reduced controllability of the airplane.

Applies to 1 model in our index